Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept
By: David J. Wing.
Contributors: Langley Research Center.
Series: NASA technical paper -- 3411.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1994
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Jet nozzles -- Testing.; Exhaust nozzles.; Nozzle geometry.; Skewness.; Sonic nozzles.; Static tests.; Throats.; Thrust vector control.; Wind tunnel tests.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 94-0821-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 2 microfiches.